US9576713B2 - Variable reluctance transducers - Google Patents

Variable reluctance transducers Download PDF

Info

Publication number
US9576713B2
US9576713B2 US14/365,196 US201314365196A US9576713B2 US 9576713 B2 US9576713 B2 US 9576713B2 US 201314365196 A US201314365196 A US 201314365196A US 9576713 B2 US9576713 B2 US 9576713B2
Authority
US
United States
Prior art keywords
magnetic
gap
magnetic structure
polymer
approximately
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active, expires
Application number
US14/365,196
Other languages
English (en)
Other versions
US20150084726A1 (en
Inventor
George David Goodman
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Halliburton Energy Services Inc
Original Assignee
Halliburton Energy Services Inc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Halliburton Energy Services Inc filed Critical Halliburton Energy Services Inc
Assigned to HALLIBURTON ENERGY SERVICES, INC. reassignment HALLIBURTON ENERGY SERVICES, INC. ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: GOODMAN, GEORGE DAVID
Assigned to HALLIBURTON ENERGY SERVICES, INC. reassignment HALLIBURTON ENERGY SERVICES, INC. ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: GOODMAN, GEORGE DAVID
Publication of US20150084726A1 publication Critical patent/US20150084726A1/en
Application granted granted Critical
Publication of US9576713B2 publication Critical patent/US9576713B2/en
Active legal-status Critical Current
Adjusted expiration legal-status Critical

Links

Images

Classifications

    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01L—MEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
    • G01L9/00—Measuring steady of quasi-steady pressure of fluid or fluent solid material by electric or magnetic pressure-sensitive elements; Transmitting or indicating the displacement of mechanical pressure-sensitive elements, used to measure the steady or quasi-steady pressure of a fluid or fluent solid material, by electric or magnetic means
    • G01L9/10—Measuring steady of quasi-steady pressure of fluid or fluent solid material by electric or magnetic pressure-sensitive elements; Transmitting or indicating the displacement of mechanical pressure-sensitive elements, used to measure the steady or quasi-steady pressure of a fluid or fluent solid material, by electric or magnetic means by making use of variations in inductance, i.e. electric circuits therefor
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01F—MAGNETS; INDUCTANCES; TRANSFORMERS; SELECTION OF MATERIALS FOR THEIR MAGNETIC PROPERTIES
    • H01F7/00—Magnets
    • H01F7/06—Electromagnets; Actuators including electromagnets
    • H01F7/08—Electromagnets; Actuators including electromagnets with armatures
    • H01F7/16—Rectilinearly-movable armatures
    • H01F7/1638—Armatures not entering the winding
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01F—MAGNETS; INDUCTANCES; TRANSFORMERS; SELECTION OF MATERIALS FOR THEIR MAGNETIC PROPERTIES
    • H01F7/00—Magnets
    • H01F7/06—Electromagnets; Actuators including electromagnets
    • H01F7/08—Electromagnets; Actuators including electromagnets with armatures
    • H01F7/121—Guiding or setting position of armatures, e.g. retaining armatures in their end position
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01L—MEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
    • G01L9/00—Measuring steady of quasi-steady pressure of fluid or fluent solid material by electric or magnetic pressure-sensitive elements; Transmitting or indicating the displacement of mechanical pressure-sensitive elements, used to measure the steady or quasi-steady pressure of a fluid or fluent solid material, by electric or magnetic means
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01F—MAGNETS; INDUCTANCES; TRANSFORMERS; SELECTION OF MATERIALS FOR THEIR MAGNETIC PROPERTIES
    • H01F7/00—Magnets
    • H01F7/06—Electromagnets; Actuators including electromagnets
    • H01F7/08—Electromagnets; Actuators including electromagnets with armatures
    • H01F7/10—Electromagnets; Actuators including electromagnets with armatures specially adapted for alternating current
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T156/00—Adhesive bonding and miscellaneous chemical manufacture
    • Y10T156/10—Methods of surface bonding and/or assembly therefor

Definitions

  • This disclosure relates to variable reluctance devices, and more particularly to a variable reluctance device for applying an oscillatory mechanical force to a load.
  • Electromagnetic transducers are widely used to convert electromagnetic energy into translational motion.
  • Common categories of transducers include moving coil designs and moving armature designs, so named for the primary moving elements of each.
  • the latter designs are often referred to as variable reluctance devices, as the magnetic reluctance, or the ratio of magnetomotive force to magnetic flux, varies as the magnetic armature moves in relation to a fixed magnetic structure.
  • Variable reluctance devices are frequently used in various applications including agitators, acoustic devices, and sensors. In these applications, a device should operate efficiently, such that large translational forces are converted efficiently from an applied excitation current. A device should also operate linearly, such that a flat translational response is produced over a broad range of excitation frequencies.
  • FIG. 1 is a schematic diagram of an example device.
  • FIGS. 2A-B are schematic diagrams of an example devices.
  • FIG. 3 shows the relationship between the gap permeability and the inductance of an example device.
  • FIGS. 4A-B show examples of fringing flux.
  • FIG. 5 shows an example sonic measurement device in a wireline configuration.
  • FIG. 6 shows an example sonic measurement device in a MWD/LWD configuration.
  • Embodiments of the present subject matter may be used to improve any of a variety of devices with dynamic magnetic gap regions. These devices may include, for example, transducers, solenoids, relays, microphones speakers, displacement sensors, magnetic sensors, and mechanical vibrators. For illustrative purposes, the following description discusses embodiments of variable reluctance devices.
  • FIG. 1 is a schematic diagram of an example embodiment of a variable reluctance device 100 .
  • Device 100 includes several magnetic structures that contain magnetic flux, and the magnetic structures are arranged to form one or more magnetic circuits.
  • device 100 includes a load structure 102 connected to an armature 104 through a connecting arm 106 .
  • Armature 104 includes two sets of I-shaped laminations 108 and 110 , oppositely disposed on armature 104 .
  • Armature 104 is positioned between two oppositely oriented core structures 112 and 114 .
  • Core structures 112 and 114 are formed from E-shaped laminations, and are positioned such that their leg portions 116 and 118 face inwardly towards armature 104 .
  • a structural frame 120 secures core structures 112 and 114 in a fixed position, such that gap region 122 is formed between the opposing outer surfaces (i.e. pole faces) of core structure 112 and lamination 108 .
  • gap region 124 is formed between the opposing outer surfaces (i.e. pole faces) of core structure 114 and lamination 110 .
  • magnetic flux between core structure 112 and lamination 108 flows through the pole face of core structure 112 , through gap region 122 , and through the pole face of lamination 108 , and vice versa, completing a magnetic circuit.
  • Armature 104 is resiliently centered between core structures 112 and 114 by a spring 126 , such that gaps 122 and 124 are approximately equal when armature 104 is at rest.
  • spring 126 also provides mechanical damping of motion of the armature 104 relative to each of the core structures 112 and 114 .
  • Core structures 112 and 114 are each wound by a first biasing winding 128 and 130 , respectively, and by a second winding 132 and 134 , respectively.
  • Biasing windings 128 and 130 are connected to a supply of direct current (DC) 136 , so that a biasing current from DC supply 136 biases the two magnetic circuits.
  • the second windings 132 and 134 are connected to a supply of alternating current (AC) 138 , so that an excitation current from AC supply 138 is applied to the two magnetic circuits.
  • DC direct current
  • AC alternating current
  • Windings 132 and 134 are installed or phased relative to the first windings 128 and 130 , such that at any given moment when AC supply 138 is energized, one of the second windings 132 or 134 aids the corresponding first winding 128 or 130 , while the other second winding 132 or 134 opposes the corresponding first winding 128 or 130 .
  • This phasing also causes any induced AC voltages in the DC windings to effectively cancel so that no substantial AC load is impressed on the DC supply.
  • energizing the device with an alternating current produces a highly non-linear force upon armature 104 , which is exerted at twice the frequency of the exciting current.
  • This force upon armature 104 correspondingly drives load 102 in an oscillating manner. Due to this oscillation, gaps 122 and 124 are dynamic, and have variable gap widths during the operation of device 100 .
  • the frequency and distance by which load 102 oscillates may vary depending on the desired oscillation characteristics of the device, the physical constraints of the particular application, and the frequency and voltage limitations of the AC power supply.
  • load 102 oscillates at a frequency between 20 Hz 20 kHz.
  • the oscillation of load 102 may be varied by the user, such as by varying the frequency of the induced AC voltage from supply 138 .
  • the oscillation of load 102 may be varied during use, such that a range of oscillation frequencies may be induced during use.
  • the widths of gaps 122 and 124 may vary.
  • the gap widths are selected so that it is large enough to allow armature 104 to freely oscillate, while narrow enough to reduce magnetic tosses due to fringing effects.
  • the static gap width i.e. the width of the gaps when armature 104 is in a steady state non-energized condition, for example when DC supply 136 and/or AC supply 138 is switched oft
  • the static gap width may vary between 0.1% to 10% of a pole face's cross-sectional length or width.
  • the gap width may be 0.5% of a pole face's cross-sectional length or width.
  • the oscillatory displacement of armature 104 within gaps 122 and 124 may also vary.
  • the maximum displacement of armature 104 is approximately 50% of the static gap width, such that in a position of maximum displacement, one gap is approximately 50% of its static width, and the other gap is approximately 150% of its static width.
  • the maximum displacement of armature 104 may be greater than or less than 50%.
  • the maximum displacement of armature 104 may vary between 0% to 80% of the static gap width.
  • Core structures 112 and 114 and armature 104 may be of various shapes and configurations. For example, these structures may be rod-shaped, plane-shaped, E-shaped, I-shaped, U-shaped, C-shaped, or any other shape.
  • Device 100 further includes a magnetic substance 140 within gaps 122 and 124 .
  • magnetic substance 140 conforms to the width of gaps 122 and 124 , and is compressed or stretched to allow movement of armature 104 .
  • FIG. 2A a leftward motion of armature 104 causes gap 122 to narrow (compressing magnetic substance 140 within it), and causes gap 124 to expand (expanding magnetic substance 140 within it).
  • FIG. 2B A rightward motion is illustrated in FIG. 2B , showing an expansion and compression of magnetic substance 140 in gaps 122 and 124 , respectively.
  • Magnetic substance may be retained within gaps 122 and 124 in various ways.
  • magnetic substance 140 is mechanically fixed within gaps 122 and 124 , for instance through an adhesive, boot, or other retaining structure.
  • magnetic substance 140 is fixed within gaps 122 and 124 through magnetic forces between substance 140 , armature 104 , and core structures 112 and 114 .
  • Magnetic substance 140 may be of any pliable or elastomeric magnetic substance, such as an elastomer with a polymer matrix impregnated with a ferromagnetic material. Suitable materials for each component may vary based on the desired mechanical and magnetic properties of the magnetic substance.
  • the polymer matrix may be of various types, for example unsaturated rubbers (such as butyl rubber, nitrile rubber, or polyisoprene), or saturated rubbers (such as ethylene propylene rubber, silicone rubber, room temperature vulcanizing (WIN) silicone rubber, and fluoroelastomer).
  • Materials may be selected based on various factors, such as their ability to accept loadings of magnetic power, and their mechanical properties, including the material's hardness, stress-strain, compression behavior, adhesion properties, viscoelasticity, stiffness, processability, vibration isolation characteristics, or other physical properties.
  • an elastomer may be selected based on its dynamic stiffness and dampening. For instance, a butyl rubber may be selected, having a dynamic spring rate of approximately 70-200%, and a damping coefficient of approximately 15-100 pounds seconds per inch (lb ⁇ s/in) within an operating temperature range of approximately 0-90° C.
  • a material such as a cis-polyisoprene elastomer may be selected, having a dynamic spring rate of approximately 70-200% and a damping coefficient of approximately 10-35 lbs/in within the same operating temperature range.
  • other materials may be chosen based on various other criteria, either instead of or in addition to these material properties. For instance, a material may be selected having a particular effective strain, such as a fluoroelastomer with an effective strain in the range of approximately 40% to 60%.
  • the ferromagnetic material may also be of various types, for example ceramic ferrites (such as barium or strontium ferrites) and rare-earth alloys such as samarium-cobalt or neodymium-iron boron). Ferromagnetic materials may vary in particle size. For example, particles may be powder-like (approximately 2 ⁇ m or less in diameter), or may be larger (such as approximately, 2-10 ⁇ in diameter, 10-300 ⁇ m in diameter, or over 300 ⁇ m in diameter). Ferromagnetic materials may be selected based on factors such as their size, initial permeability, saturation flux density, relative loss factor, resistivity, density, cost, or other factors.
  • a ferromagnetic material may be selected based on its initial permeability. For instance, a manganese-zinc (MnZn) ferrite powder may be selected, having an initial relative permeability of approximately 1000-15,000. If instead a material is needed with a lower initial permeability, a material such as a nickel-zinc (NiZn) ferrite powder may be selected, having an initial relative permeability of approximately 100-1500. In a similar manner, other materials may be chosen based on various other criteria, either instead of or in addition to these material properties.
  • MnZn manganese-zinc
  • NiZn nickel-zinc
  • magnetic substance 140 is a polymer-ferrite composite that includes a synthetic fluoropolymer elastomer fluoroelastomer (such as that commonly sold under the brand name DuPont Viton AL-600), impregnated with a high temperature nickel-zinc (NiZn) ferrite dust (such as that commonly sold under the brand name Unimagnet UR1K).
  • a synthetic fluoropolymer elastomer fluoroelastomer such as that commonly sold under the brand name DuPont Viton AL-600
  • NiZn nickel-zinc
  • Viton AL-600 is a terpolymer of hexafluoropropylene, vinylidene fluoride and tetrafluoroethylene, and is composed of approximately 98% 1-Propene, 1,1,2,3,3,3-hexafluoro-, polymer with 1,1-difluoroethene and tetrafluoroethene, and approximately 1% barium sulfate.
  • Viton AL-600 exhibits a specific gravity of 1.77, and a nominal Mooney viscosity (ML 1+10 at 121° C.) of 60.
  • Other elastomers may also be used, either in addition to or instead of Viton.
  • Ferrite dust UR1K is a soft ferrite material that is composed, in part, of NiZn magnetic material. Ferrite dust UR1K exhibits an initial permeability ( ⁇ i ) of approximately 1000 ⁇ 20%, a saturation flux density B s of approximately 350 mT, a relatively loss factor (tan ⁇ / ⁇ i ) of less than approximately 40 ⁇ 10 ⁇ 6 , a relative temperature coefficient ( ⁇ ) of less than 5 ⁇ 10 ⁇ 6 /K, a Curie temperature (T c ) of less than 120° C., a resistivity ( ⁇ ) of approximately 100,000 ⁇ m, and a density d of approximately 5 ⁇ 10 3 kg/m 3 . In general, other ferromagnetic materials may be used where the initial permeability ⁇ i is approximately 50 or greater.
  • the composition of magnetic substance 140 may be varied in order to achieve the desired physical and magnetic properties.
  • magnetic substance 140 includes approximately 60% Viton and 40% ferrite dust UR1K, resulting in a net initial permeability of approximately 8.
  • magnetic substance 140 includes a greater percentage of ferrite, in order to increase the initial permeability of substance 140 .
  • magnetic substance 140 may include approximately 50% Viton and 50% ferrite dust, resulting in a magnetic substance 140 that is firmer and exhibits a higher magnetic permeability.
  • magnetic substance 140 includes greater amounts of the non-magnetic materials, in order to increase the elasticity, deformability, or other physical characteristics of substance 140 .
  • magnetic substance 140 may include approximately 80% Viton and 20% ferrite dust, resulting in a magnetic substance 140 that exhibits greater elasticity and lower magnetic permeability.
  • certain embodiments of magnetic substance 140 may contain between 20% to 97% elastomer (e.g. approximately 20%, 30%, 40%, 50%, 60%, 70%, 80%, or 90% elastomer) and between 3% to 80% of a magnetic material (e.g. approximately 10%, 20%, 30%, 40%, 50%, 60%, 70%, or 80% of a magnetic material). In this manner, the physical and magnetic properties of substance 140 may be adjusted to suit any specific application.
  • magnetic substance 140 may contain additional materials to further alter the physical or magnetic properties of substance 140 . In this manner, the physical and magnetic properties of substance 140 may be further adjusted to sun a particular application.
  • Filing gaps 122 and 124 with a magnetic substance increases the magnetic permeability of the gap region.
  • the reluctance of a magnetic circuit is defined as the ratio of the magnetic path length to its cross sectional area divided by permeability. Inductance is the reciprocal of reluctance. As reluctances combine linearly over a magnetic circuit path, the performance of a variable reluctance device with air-filled magnetic gap regions may be compared to that of a variable reluctance device with magnetic gap regions Idled with a magnetic substance through the following relationship:
  • L air N 2 ⁇ A c ⁇ ⁇ 0 ⁇ ⁇ core l core + 4 ⁇ l g ⁇ ⁇ core
  • ⁇ L m N 2 ⁇ A c ⁇ ⁇ m ⁇ ⁇ 0 ⁇ ⁇ core l core ⁇ ⁇ m + 4 ⁇ l g ⁇ ⁇ core
  • L m L air ⁇ m ⁇ ( l core + 4 ⁇ l g ⁇ ⁇ core ) 4 ⁇ l g ⁇ ⁇ core + l core ⁇ ⁇ m
  • L air is the coil inductance with an air-filled magnetic gap region
  • L m is the coil inductance with a magnetic substance in the magnetic gap region
  • N is the total turns in windings of the coil
  • a c is the magnetic cross sectional area of the gap
  • ⁇ o is the permeability of free space
  • ⁇ m is the relative permeability of the magnetic substance
  • ⁇ core is the relative permeability of the
  • the net gain in inductance is approximately equal to the product of the gap material's relative permeability and the device's initial inductance with only air filled gap regions.
  • the inductance of the device increases 19.3 times when the air gap regions are filled by a magnetic substance with a relative permeability 20 times that of free space.
  • magnetic substance 140 in gaps 122 and 124 increases the force that is applied upon armature 104 for a given excitation current applied to the windings 132 and 134 . Thus, a greater amount of force is applied to armature 104 per ampere of excitation current.
  • magnetic substance 140 in gaps 122 and 124 decreases the number of windings around core structures 112 and 114 that are needed to achieve a particular force.
  • Device designs with fewer coil windings reduce the volume and mass requirements for the coils, and as a result, may also reduce the manufacturing cost of the devices while increasing reliability.
  • magnetic substance 140 improves the mechanical dampening of the movement of armature 104 by physically opposing the motion of the armature 104 . This dampening effect may result in a flatter, more linear force response as a function of excitation frequency. Thus, the amount of force applied to armature 104 per ampere of excitation current is relatively consistent over a range of frequencies of the excitation current.
  • magnetic substance 140 provides gap equalization for gaps 122 and 124 , or centralization of armature 104 within these gaps.
  • magnetic substance 140 may be deformable, such that it may be compressed when armature 104 is forced towards a core structure 112 or 114 .
  • magnetic substance 140 may return to a pre-determined shape with pre-determined dimensions when the force is removed.
  • magnetic substance 140 may be used to center armature 140 between core structures 112 and 114 .
  • magnetic substance 140 is in a compressed positive pressure state, even when gap 122 or 124 is at its maximum width.
  • magnetic substance 140 fills gaps 122 and 124 , either partially or entirely, at all times, along the entire range of motion of armature 104 .
  • the opposing forces of compressed magnetic substance 140 may also center armature 104 between core structures 112 and 114 .
  • magnetic substance 140 reduces electrical losses due to fringing flux in the dynamic gap region between magnetic poles.
  • magnetic circuits are prone to flux leakage problems, as magnetic flux is very pervasive when it encounters a reluctance discontinuity along its magnetic path.
  • the flux that leaks from its intended path in this manner is termed fringing flux, and is the most pervasive for large air-filled gaps.
  • fringing flux The flux that leaks from its intended path in this manner.
  • the fraction of total gap induced fringing flux can be estimated using the following equation:
  • Fringing ⁇ ⁇ Flux l g A c ⁇ ln ⁇ ( 2 ⁇ G l g ) , where G is the mean magnetic path length, l g is the length of the gap, and A c is cross sectional area of the magnetic material.
  • G the mean magnetic path length
  • l g the length of the gap
  • a c cross sectional area of the magnetic material.
  • the nominal fringing flux is approximately 7.4%, with up to 10.4% flux lost to fringing at maximum mechanical displacement. Flux that escapes the intended magnetic path is free to impinge on other magnetic structures and conductive surfaces, inducing undesirable eddy currents. Fringing flux thus induces undesirable force vector components on the device's moving elements.
  • the preferred flux direction is normal to the pole faces that form the gap. As illustrated in FIG. 4A , the preferred flux direction is along the x-axis. However, as the fringing flux expands outward from its intended magnetic path, it takes orthogonal components falling in both the y-axis and z-axis directions. As a result, undesirable response modes are generated by the device. When permeable material is introduced within the gap, the magnetic flux becomes much more contained. For example, in an embodiment where the relative permeability of the magnetic substance is more than 10 times that of free space, much less flux falls outside of its intended path, as illustrated in FIG. 4B .
  • magnetic substance 140 reduces orthogonal force components resulting from fringing flux in the magnetic pole region, thereby reducing its negative effects upon the oscillatory motion of the armature 104 as it oscillates between core structures 112 and 114 .
  • magnetic substance 140 provides mechanical dampening of force components that oppose the device's oscillatory movement performance.
  • magnetic substance 140 may reduce orthogonal forces or shear forces, such as those that arise when magnetic substance 140 is under compression.
  • dampening may be desirable in certain other circumstances, for instance to ensure that the oscillatory motion of armature 104 is rapidly ceased when excitation current is removed from windings 132 and 134 .
  • dampening may also reduce unwanted resonant behavior of device 100 .
  • magnetic substance 140 may be selected based on physical parameters that to provide specific mechanical dampening properties to device 100 . For instance, the elasticity or the hardness of the substance 140 may be selected to supplement the resistive forces of the mechanical spring 126 of device 100 .
  • magnetic substance 140 reduces the device's dependence on spring 126 when an elastic gap material is selected, such that armature 104 is resiliently centered by both magnetic substance 140 and the spring 126 .
  • spring 126 is removed entirely, and armature 104 is resiliently centered between core structures 112 and 114 entirely by magnetic substance 140 .
  • magnetic substance 140 provides a physical separation between armature 104 and core structures 112 and 114 , thereby eliminating discontinuities in the magnetic circuit that would occur if armature 104 contacts either core structure 112 or 114 .
  • gap regions 122 and 124 are preserved during operation of device 100 , ensuring the continued operation of device 100 .
  • the physical separation provided by magnetic substance 140 ensures that armature 104 will not contact either core structure 112 and 114 , thereby preventing damage that arises from physical contact between components.
  • variable reluctance devices where the dynamic gap regions of the device are filled with a magnetic, material in order to improve the device's operating characteristics.
  • These variable reluctance devices may be used in conjunction with various systems for a variety of applications.
  • embodiments can be used in acoustic and sonic measurement tools, such as those commonly used in oilfield drilling and/or formation evaluation applications.
  • an example sonic measurement tool 500 can be used in a wireline configuration.
  • Tool 500 includes multiple variable reluctance transducers 502 arranged in a multiple element array.
  • Sonic measurement tool 500 is suspended over a well using a support structure 562 , and may be lowered into a welt 550 , for example by extending a support cable 552 or other drill string structure.
  • transducers 502 may be used as high amplitude transmitters to generate and direct acoustic energy 504 in specific shear and compressional modes into a surrounding medium 554 .
  • Receivers 506 arranged in a multiple element array on tool 500 , detect energy that is reflected by the medium 554 . Based on energy reflected by the medium, measurement tool 500 assesses and records the physical properties of a surrounding medium.
  • Measurements from tool 500 may be transmitted through support cable 552 to a surface control system 560 , where the measurements are reviewed by an operator. In some embodiments, either additionally or alternatively, measurements may be stored within tool 500 (e.g. in a data storage device) for future retrieval and review at the surface. Embodiments of this technology may be used to improve measurement tool 500 in various ways. For instance, one or more devices 100 could be disposed within each transducer 502 , such that transducers 502 may be built smaller than transducers having air-fi lied dynamic gap regions. Thus, a tool 500 that includes transducers 502 may be built smaller with similar performance characteristics.
  • embodiments of this technology may be used to improve the linearity of the acoustic response of transducers 502 , and increase the acoustic energy produced by transducers 502 , thereby increasing the performance and power efficiency of transducers 502 .
  • a sonic measurement tool 600 can be used in a MWD/LWD configuration.
  • a drill unit 602 and the tool 600 are attached to a drill string 604 .
  • a surface control unit 606 an operator may direct a drill unit 602 along a three dimensional path, creating a borehole 608 .
  • the operator may use tool 600 to assess and record the physical properties of a surrounding medium 610 .
  • Tool 600 includes one or more transducers 620 , which may be used as high amplitude transmitters to generate and direct acoustic energy 622 in specific shear and compressional modes into a surrounding medium 610 .
  • One or more receivers 624 are arranged on tool 600 to detect energy that is reflected by the medium 610 . Based on energy reflected by the medium, measurement tool 600 assesses and records the physical properties of the surrounding medium 610 . Measurements from tool 600 may be transmitted through drill string 604 to a surface control system 606 , where they are reviewed by an operator. Additionally or alternatively, measurements may be stored within tool 600 (e.g. in a data storage device) for future retrieval and review at the surface. In this manner, an operator may use a surface control unit 602 to direct the operation of a drill unit 602 , white using tool 600 to repeatedly assess medium 610 . Embodiments of this technology may be used to improve measurement tool 600 in various ways.
  • transducer 602 may be smaller, produce more acoustic energy, and/or may be more efficient than transducers having air-filled dynamic gap regions
  • embodiments of this technology can be used in a wide variety of drilling and/or formation evaluation applications, such as with transducers or variable reluctance devices used in wireline, slickline, coiled tubing, measurement while drilling (MWD), logging while drilling (LWD) operations.
  • transducers or variable reluctance devices used in wireline, slickline, coiled tubing, measurement while drilling (MWD), logging while drilling (LWD) operations.
  • a compressible magnetic material may be added to the gap regions of devices such as relays, solenoids, microphones, speakers, displacement sensors, magnetic sensors, and mechanical vibrators, in order to increase the magnetic permeability of the gap region and to provide varying degrees of mechanical damping.
  • the magnetic structures do not continuously oscillate relative to one another. Instead, each magnetic structure may have windings connected only to one or more DC sources. When a DC current is applied to windings of one or more of the magnetic structures, this causes the magnetic structures to change state relative to one another. That is, one magnetic structure may move closer to or further from the other, changing the width of the dynamic magnetic gap.
  • the dynamic magnetic gap may be filled with a magnetic polymer in order to increase magnetic permeability of the gap region, reduce fringing flux, and increase mechanical damping.
  • the example device may be several different states, such that the magnetic structures may move between several defined positions relative to one another, for instance in a double throw switch configuration.
  • a compressible magnetic material may be added to any device with a dynamic air gap formed between two or more opposing magnetic structures, where an increase in magnetic permeability, a reduction of fringing flux, and an increase in mechanical dampening are beneficial. Accordingly, other embodiments are within the scope of the following claims.

Landscapes

  • Physics & Mathematics (AREA)
  • Electromagnetism (AREA)
  • Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • General Physics & Mathematics (AREA)
  • Vibration Prevention Devices (AREA)
  • Reciprocating, Oscillating Or Vibrating Motors (AREA)
  • Electromagnets (AREA)
  • Manufacturing & Machinery (AREA)
US14/365,196 2013-08-26 2013-08-26 Variable reluctance transducers Active 2033-12-28 US9576713B2 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/US2013/056664 WO2015030709A1 (en) 2013-08-26 2013-08-26 Variable reluctance transducers

Publications (2)

Publication Number Publication Date
US20150084726A1 US20150084726A1 (en) 2015-03-26
US9576713B2 true US9576713B2 (en) 2017-02-21

Family

ID=52587077

Family Applications (1)

Application Number Title Priority Date Filing Date
US14/365,196 Active 2033-12-28 US9576713B2 (en) 2013-08-26 2013-08-26 Variable reluctance transducers

Country Status (5)

Country Link
US (1) US9576713B2 (es)
EP (1) EP3005540A1 (es)
AU (1) AU2013399148B2 (es)
MX (1) MX351734B (es)
WO (1) WO2015030709A1 (es)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10720823B1 (en) * 2016-01-15 2020-07-21 University Of Southern California Ferrofluid liquid spring with magnets between coils inside an enclosed chamber for vibration energy harvesting
US20200412225A1 (en) * 2019-06-29 2020-12-31 AAC Technologies Pte. Ltd. Vibration Motor
US20220360198A1 (en) * 2021-05-05 2022-11-10 Enervibe Ltd Electromagnetic vibration and energy harvester having vibrating body, magnets and stationary magnet and hinge

Citations (48)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2434337A (en) * 1942-07-02 1948-01-13 Vibro Plus Corp Electromagnetic vibration motor
US2696592A (en) 1951-05-05 1954-12-07 Stewart Warner Corp Vibration pickup
US2903673A (en) 1954-01-06 1959-09-08 Harris Transducer Corp Acoustical impedance-matching transducer
US3004178A (en) 1958-06-20 1961-10-10 Ling Temco Electronics Inc Vibration generator
US3018467A (en) 1955-11-07 1962-01-23 Harris Transducer Corp Resonant reactively operating variable position transducer
US3048815A (en) 1952-11-05 1962-08-07 Edward G Thurston Low frequency transducer
US3274538A (en) 1960-09-19 1966-09-20 Benjamin L Snavely Electroacoustic transducer
US3308423A (en) 1963-12-30 1967-03-07 Dynamics Corp America Electroacoustic transducer
US3435393A (en) 1967-01-26 1969-03-25 Abex Corp Null adjustor for magnetically operated torque motors
US3439198A (en) 1965-12-27 1969-04-15 Robert H Lee Electrical actuator having a mechanical output
US3464057A (en) 1967-10-10 1969-08-26 Sanders Associates Inc Spherical directional hydrophone with semispherical magnets
US3538358A (en) * 1967-11-13 1970-11-03 Moser Gmbh Kuno Oscillating armature motor
US3872333A (en) 1972-03-08 1975-03-18 Commissariat Energie Atomique Generator for producing rectilinear vibrations at a controlled velocity especially for use in Mossbauer spectrometery
US4048602A (en) 1975-06-30 1977-09-13 Diamantides Nick D Universal impedance power apparatus
US4110731A (en) 1976-12-30 1978-08-29 Bell & Howell Company Vibration transducer with improved viscous damping
GB1599506A (en) 1977-04-09 1981-10-07 Licentia Gmbh Dynamic transducer
US4303806A (en) 1977-09-09 1981-12-01 Licentia Patent-Verwaltungs-G.M.B.H. Dynamic electroacoustic transducer having a moving coil in an air gap filled with a magnetic liquid
US4308603A (en) 1979-11-16 1981-12-29 The United States Of America As Represented By The Secretary Of The Navy Ferrofluid transducer
US4361879A (en) 1980-08-25 1982-11-30 The United States Of America As Represented By The Secretary Of The Navy Ferrofluid transducer
US4742998A (en) 1985-03-26 1988-05-10 Barry Wright Corporation Active vibration isolation system employing an electro-rheological fluid
US5266854A (en) 1990-08-30 1993-11-30 Bolt Beranek And Newman Inc. Electromagnetic transducer
US5267737A (en) 1992-01-16 1993-12-07 International Business Machines, Corp. Magnetic fluid seal containment shield
US5280260A (en) * 1992-08-13 1994-01-18 Eaton Corporation Rotary solenoid utilizing concurrently energized AC and DC coils
US5281939A (en) * 1993-05-28 1994-01-25 Eaton Corporation Multiple pole solenoid using simultaneously energized AC and DC coils
US5445249A (en) 1993-02-18 1995-08-29 Kabushiki Kaisha Toshiba Dynamic vibration absorber
US5621293A (en) * 1991-11-26 1997-04-15 Hutchinson Variable-reluctance servocontrolled linear motor
DE19805455A1 (de) * 1997-02-28 1998-09-03 Fev Motorentech Gmbh & Co Kg Elektromagnetischer Aktuator mit magnetischer Auftreffdämpfung
US5808839A (en) 1994-09-13 1998-09-15 Seagate Technology, Inc. Disc drive cartridge including magnetic bearings
WO1998048195A2 (en) 1997-04-24 1998-10-29 Bell Helicopter Textron Inc. Magnetic particle damper apparatus
US5896076A (en) * 1997-12-29 1999-04-20 Motran Ind Inc Force actuator with dual magnetic operation
US5973422A (en) 1998-07-24 1999-10-26 The Guitammer Company Low frequency vibrator
US6095486A (en) 1997-03-05 2000-08-01 Lord Corporation Two-way magnetorheological fluid valve assembly and devices utilizing same
US6208743B1 (en) 1996-03-21 2001-03-27 Sennheiser Electronic Gmbh & Co. K.G. Electrodynamic acoustic transducer with magnetic gap sealing
WO2001039588A1 (en) * 1999-12-06 2001-06-07 Macrosonix Corporation High stability dynamic force reluctance motor
WO2002039781A2 (en) 2000-11-08 2002-05-16 New Transducers Limited Loudspeaker driver
JP2002177882A (ja) 2000-12-07 2002-06-25 Nidec Copal Corp 振動発生器
US6555229B1 (en) * 2000-04-24 2003-04-29 Nexpress Solutions Llc Fluorocarbon-silicone random copolymer for use in toner release layer
US6879076B2 (en) 2002-12-09 2005-04-12 Johnny D. Long Ellipsoid generator
US7288860B2 (en) 2002-02-19 2007-10-30 Teledyne Licensing, Inc. Magnetic transducer with ferrofluid end bearings
US7576454B2 (en) 2005-05-23 2009-08-18 Ciiis, Llc Multiple magnet coil in gap generator
WO2011047801A1 (de) * 2009-10-20 2011-04-28 Eto Magnetic Gmbh Monostabile elektromagnetische aktuatorvorrichtung
US20110133488A1 (en) 2008-04-15 2011-06-09 Stephen Roberts Electromechanical Generator for, and Method of, Converting Mechanical Vibrational Energy Into Electrical Energy
US7990136B2 (en) 2002-10-07 2011-08-02 Moving Magent Technologies Variable reluctance position sensor
US20110278963A1 (en) 2008-11-18 2011-11-17 Institut fuer Luft-und Kaeltetechnik gemeinnuetzige GmbH Electrodynamic Linear Oscillating Motor
US20120211316A1 (en) 2011-02-22 2012-08-23 National Taipei University Of Technology Magneto-rheological fluid damper
US8280096B2 (en) 2007-08-09 2012-10-02 Gilles Milot Electrodynamic transducer, in particular of the loudspeaker type with ferrofluid suspension and related devices
US8279031B2 (en) 2011-01-20 2012-10-02 Correlated Magnetics Research, Llc Multi-level magnetic system for isolation of vibration
KR20130025636A (ko) 2011-09-02 2013-03-12 삼성전기주식회사 진동발생장치

Patent Citations (49)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2434337A (en) * 1942-07-02 1948-01-13 Vibro Plus Corp Electromagnetic vibration motor
US2696592A (en) 1951-05-05 1954-12-07 Stewart Warner Corp Vibration pickup
US3048815A (en) 1952-11-05 1962-08-07 Edward G Thurston Low frequency transducer
US2903673A (en) 1954-01-06 1959-09-08 Harris Transducer Corp Acoustical impedance-matching transducer
US3018467A (en) 1955-11-07 1962-01-23 Harris Transducer Corp Resonant reactively operating variable position transducer
US3004178A (en) 1958-06-20 1961-10-10 Ling Temco Electronics Inc Vibration generator
US3274538A (en) 1960-09-19 1966-09-20 Benjamin L Snavely Electroacoustic transducer
US3308423A (en) 1963-12-30 1967-03-07 Dynamics Corp America Electroacoustic transducer
US3439198A (en) 1965-12-27 1969-04-15 Robert H Lee Electrical actuator having a mechanical output
US3435393A (en) 1967-01-26 1969-03-25 Abex Corp Null adjustor for magnetically operated torque motors
US3464057A (en) 1967-10-10 1969-08-26 Sanders Associates Inc Spherical directional hydrophone with semispherical magnets
US3538358A (en) * 1967-11-13 1970-11-03 Moser Gmbh Kuno Oscillating armature motor
US3872333A (en) 1972-03-08 1975-03-18 Commissariat Energie Atomique Generator for producing rectilinear vibrations at a controlled velocity especially for use in Mossbauer spectrometery
US4048602A (en) 1975-06-30 1977-09-13 Diamantides Nick D Universal impedance power apparatus
US4110731A (en) 1976-12-30 1978-08-29 Bell & Howell Company Vibration transducer with improved viscous damping
GB1599506A (en) 1977-04-09 1981-10-07 Licentia Gmbh Dynamic transducer
US4303806A (en) 1977-09-09 1981-12-01 Licentia Patent-Verwaltungs-G.M.B.H. Dynamic electroacoustic transducer having a moving coil in an air gap filled with a magnetic liquid
US4308603A (en) 1979-11-16 1981-12-29 The United States Of America As Represented By The Secretary Of The Navy Ferrofluid transducer
US4361879A (en) 1980-08-25 1982-11-30 The United States Of America As Represented By The Secretary Of The Navy Ferrofluid transducer
US4742998A (en) 1985-03-26 1988-05-10 Barry Wright Corporation Active vibration isolation system employing an electro-rheological fluid
US5266854A (en) 1990-08-30 1993-11-30 Bolt Beranek And Newman Inc. Electromagnetic transducer
US5621293A (en) * 1991-11-26 1997-04-15 Hutchinson Variable-reluctance servocontrolled linear motor
US5267737A (en) 1992-01-16 1993-12-07 International Business Machines, Corp. Magnetic fluid seal containment shield
US5280260A (en) * 1992-08-13 1994-01-18 Eaton Corporation Rotary solenoid utilizing concurrently energized AC and DC coils
US5445249A (en) 1993-02-18 1995-08-29 Kabushiki Kaisha Toshiba Dynamic vibration absorber
US5281939A (en) * 1993-05-28 1994-01-25 Eaton Corporation Multiple pole solenoid using simultaneously energized AC and DC coils
US5808839A (en) 1994-09-13 1998-09-15 Seagate Technology, Inc. Disc drive cartridge including magnetic bearings
US6208743B1 (en) 1996-03-21 2001-03-27 Sennheiser Electronic Gmbh & Co. K.G. Electrodynamic acoustic transducer with magnetic gap sealing
DE19805455A1 (de) * 1997-02-28 1998-09-03 Fev Motorentech Gmbh & Co Kg Elektromagnetischer Aktuator mit magnetischer Auftreffdämpfung
US6095486A (en) 1997-03-05 2000-08-01 Lord Corporation Two-way magnetorheological fluid valve assembly and devices utilizing same
WO1998048195A2 (en) 1997-04-24 1998-10-29 Bell Helicopter Textron Inc. Magnetic particle damper apparatus
US5896076A (en) * 1997-12-29 1999-04-20 Motran Ind Inc Force actuator with dual magnetic operation
US5973422A (en) 1998-07-24 1999-10-26 The Guitammer Company Low frequency vibrator
WO2001039588A1 (en) * 1999-12-06 2001-06-07 Macrosonix Corporation High stability dynamic force reluctance motor
US6388417B1 (en) 1999-12-06 2002-05-14 Macrosonix Corporation High stability dynamic force motor
US6555229B1 (en) * 2000-04-24 2003-04-29 Nexpress Solutions Llc Fluorocarbon-silicone random copolymer for use in toner release layer
WO2002039781A2 (en) 2000-11-08 2002-05-16 New Transducers Limited Loudspeaker driver
JP2002177882A (ja) 2000-12-07 2002-06-25 Nidec Copal Corp 振動発生器
US7288860B2 (en) 2002-02-19 2007-10-30 Teledyne Licensing, Inc. Magnetic transducer with ferrofluid end bearings
US7990136B2 (en) 2002-10-07 2011-08-02 Moving Magent Technologies Variable reluctance position sensor
US6879076B2 (en) 2002-12-09 2005-04-12 Johnny D. Long Ellipsoid generator
US7576454B2 (en) 2005-05-23 2009-08-18 Ciiis, Llc Multiple magnet coil in gap generator
US8280096B2 (en) 2007-08-09 2012-10-02 Gilles Milot Electrodynamic transducer, in particular of the loudspeaker type with ferrofluid suspension and related devices
US20110133488A1 (en) 2008-04-15 2011-06-09 Stephen Roberts Electromechanical Generator for, and Method of, Converting Mechanical Vibrational Energy Into Electrical Energy
US20110278963A1 (en) 2008-11-18 2011-11-17 Institut fuer Luft-und Kaeltetechnik gemeinnuetzige GmbH Electrodynamic Linear Oscillating Motor
WO2011047801A1 (de) * 2009-10-20 2011-04-28 Eto Magnetic Gmbh Monostabile elektromagnetische aktuatorvorrichtung
US8279031B2 (en) 2011-01-20 2012-10-02 Correlated Magnetics Research, Llc Multi-level magnetic system for isolation of vibration
US20120211316A1 (en) 2011-02-22 2012-08-23 National Taipei University Of Technology Magneto-rheological fluid damper
KR20130025636A (ko) 2011-09-02 2013-03-12 삼성전기주식회사 진동발생장치

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
Greper et al., "Problems in the utilization of magnetic fluid in electrodynamic loudspeaker heads", Magnetohydrodynamics , vol. 25, No. 2, Oct. 1989, 8 pages.
International Search Report and Written Opinion of the International Searching Authority issued in International Application No. PCT/US2013/056664 on May 27, 2014; 9 pages.

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10720823B1 (en) * 2016-01-15 2020-07-21 University Of Southern California Ferrofluid liquid spring with magnets between coils inside an enclosed chamber for vibration energy harvesting
US20200412225A1 (en) * 2019-06-29 2020-12-31 AAC Technologies Pte. Ltd. Vibration Motor
US11641152B2 (en) * 2019-06-29 2023-05-02 AAC Technologies Pte. Ltd. Vibration motor with elastic connector shaft holding pole plate with magnets moving in at least two directions and coils on housing walls
US20220360198A1 (en) * 2021-05-05 2022-11-10 Enervibe Ltd Electromagnetic vibration and energy harvester having vibrating body, magnets and stationary magnet and hinge
US11581828B2 (en) * 2021-05-05 2023-02-14 Enervibe Ltd Electromagnetic vibration and energy harvester having vibrating body, magnets and stationary magnet and hinge

Also Published As

Publication number Publication date
MX351734B (es) 2017-10-26
AU2013399148B2 (en) 2017-03-23
EP3005540A1 (en) 2016-04-13
WO2015030709A1 (en) 2015-03-05
AU2013399148A1 (en) 2016-01-28
US20150084726A1 (en) 2015-03-26
MX2016000981A (es) 2016-07-19

Similar Documents

Publication Publication Date Title
US10291107B2 (en) Power generator, power generator set and power generation system
EP1101273B1 (en) Low frequency vibrator
US4845450A (en) Self-biased modular magnetostrictive driver and transducer
EP2550724B1 (en) Electromechanical conversion system with moving magnets; acoustic diffuser comprising said system and a moving member that generates sound waves
US9576713B2 (en) Variable reluctance transducers
US20180229270A1 (en) Linear vibration motor
JP2014530104A (ja) 振動トランスデューサおよびアクチュエータ
JP2012039824A (ja) 振動発電機
KR101184502B1 (ko) 선형 진동자
WO2015162988A1 (ja) 発電装置
WO2018157515A1 (zh) 用于线性振动马达的壳体以及线性振动马达
CN110557000B (zh) 振动发电机装置和鸣响装置
US1871739A (en) Driving unit for sound reproducers
KR100890713B1 (ko) 역자기 변형성을 이용한 음향 발생 장치
US2025041A (en) Electromagnetic vibrator
JP6422354B2 (ja) 発電装置
WO2022054036A3 (fr) Système emat pour la détection de discontinuités de surface et internes dans des structures conductrices à haute température
JP2007158911A (ja) 音響放射装置用電磁変換装置
WO2014168008A1 (ja) 発電装置
US20200188956A1 (en) Vibration source
US2434285A (en) Compressional wave translating device
JP2011146605A (ja) 電気機器
US11177697B1 (en) Resonant frequency power generator
JPH11135321A (ja) 電磁ソレノイド
US2705313A (en) Magnetostriction oscillator

Legal Events

Date Code Title Description
AS Assignment

Owner name: HALLIBURTON ENERGY SERVICES, INC., TEXAS

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:GOODMAN, GEORGE DAVID;REEL/FRAME:031094/0787

Effective date: 20130823

AS Assignment

Owner name: HALLIBURTON ENERGY SERVICES, INC., TEXAS

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:GOODMAN, GEORGE DAVID;REEL/FRAME:033107/0054

Effective date: 20130823

FEPP Fee payment procedure

Free format text: PAYOR NUMBER ASSIGNED (ORIGINAL EVENT CODE: ASPN); ENTITY STATUS OF PATENT OWNER: LARGE ENTITY

STCF Information on status: patent grant

Free format text: PATENTED CASE

CC Certificate of correction
MAFP Maintenance fee payment

Free format text: PAYMENT OF MAINTENANCE FEE, 4TH YEAR, LARGE ENTITY (ORIGINAL EVENT CODE: M1551); ENTITY STATUS OF PATENT OWNER: LARGE ENTITY

Year of fee payment: 4

MAFP Maintenance fee payment

Free format text: PAYMENT OF MAINTENANCE FEE, 8TH YEAR, LARGE ENTITY (ORIGINAL EVENT CODE: M1552); ENTITY STATUS OF PATENT OWNER: LARGE ENTITY

Year of fee payment: 8